Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe319-il-100000 Airfoil,goe319-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,53.33 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe319-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.2401,0.10016,0.09566,-0.0278,1.0000,0.0715 -7.750,-0.2643,0.10062,0.09627,-0.0229,1.0000,0.0717 -7.500,-0.2930,0.10149,0.09728,-0.0176,1.0000,0.0717 -7.250,-0.2879,0.09955,0.09537,-0.0226,0.9932,0.0734 -7.000,-0.2519,0.09639,0.09209,-0.0459,0.9760,0.0751 -6.750,-0.2313,0.09028,0.08605,-0.0414,0.9736,0.0763 -6.500,-0.2023,0.08588,0.08163,-0.0442,0.9685,0.0784 -6.250,-0.1742,0.08213,0.07786,-0.0500,0.9592,0.0817 -6.000,-0.1279,0.07984,0.07525,-0.0712,0.9443,0.0870 -5.750,-0.1045,0.07380,0.06936,-0.0697,0.9415,0.0885 -5.500,-0.0800,0.07031,0.06587,-0.0714,0.9334,0.0909 -5.250,-0.0464,0.06687,0.06236,-0.0770,0.9255,0.0954 -5.000,-0.0088,0.06447,0.05964,-0.0875,0.9128,0.1008 -4.750,0.0158,0.06016,0.05543,-0.0879,0.9072,0.1031 -4.500,0.0355,0.05779,0.05303,-0.0886,0.8962,0.1067 -4.250,0.0784,0.05554,0.05041,-0.0963,0.8885,0.1157 -4.000,0.0903,0.05264,0.04763,-0.0945,0.8768,0.1182 -3.750,0.1275,0.05186,0.04643,-0.0988,0.8683,0.1310 -3.500,0.1405,0.04832,0.04308,-0.0974,0.8580,0.1337 -3.250,0.1649,0.04636,0.04105,-0.0978,0.8500,0.1418 -3.000,0.1885,0.04438,0.03893,-0.0986,0.8397,0.1509 -2.750,0.2156,0.04321,0.03751,-0.0996,0.8309,0.1654 -2.500,0.2353,0.04087,0.03525,-0.0988,0.8220,0.1725 -2.250,0.2592,0.03925,0.03351,-0.0989,0.8135,0.1874 -2.000,0.2828,0.03768,0.03185,-0.0987,0.8046,0.2050 -1.750,0.3066,0.03637,0.03040,-0.0986,0.7962,0.2328 -0.250,0.4928,0.02726,0.01920,-0.0955,0.7344,0.1329 0.000,0.5232,0.02626,0.01776,-0.0944,0.7258,0.1133 0.250,0.5506,0.02512,0.01649,-0.0937,0.7166,0.1104 0.500,0.5778,0.02441,0.01560,-0.0929,0.7075,0.1099 0.750,0.6058,0.02362,0.01465,-0.0920,0.6982,0.1085 1.000,0.6323,0.02305,0.01397,-0.0911,0.6882,0.1077 1.250,0.6605,0.02238,0.01318,-0.0901,0.6792,0.1086 1.500,0.6857,0.02202,0.01280,-0.0891,0.6680,0.1113 1.750,0.7138,0.02133,0.01207,-0.0882,0.6598,0.1184 2.000,0.7378,0.02111,0.01189,-0.0871,0.6476,0.1274 2.250,0.7648,0.02071,0.01145,-0.0862,0.6371,0.1427 2.500,0.8060,0.01835,0.01068,-0.0877,0.6258,1.0000 2.750,0.8305,0.01844,0.01056,-0.0866,0.6121,1.0000 3.000,0.8557,0.01847,0.01042,-0.0855,0.5985,1.0000 3.250,0.8815,0.01847,0.01025,-0.0846,0.5848,1.0000 3.500,0.9074,0.01847,0.01008,-0.0836,0.5702,1.0000 3.750,0.9326,0.01852,0.00997,-0.0826,0.5541,1.0000 4.000,0.9569,0.01864,0.00996,-0.0815,0.5357,1.0000 4.250,0.9805,0.01882,0.01000,-0.0803,0.5157,1.0000 4.500,1.0041,0.01906,0.01009,-0.0792,0.4952,1.0000 4.750,1.0278,0.01936,0.01022,-0.0782,0.4754,1.0000 5.000,1.0513,0.01973,0.01042,-0.0772,0.4569,1.0000 5.250,1.0746,0.02015,0.01071,-0.0763,0.4399,1.0000 5.500,1.0977,0.02062,0.01106,-0.0754,0.4243,1.0000 5.750,1.1208,0.02113,0.01149,-0.0746,0.4105,1.0000 6.000,1.1443,0.02168,0.01194,-0.0738,0.3986,1.0000 6.500,1.1913,0.02281,0.01292,-0.0724,0.3773,1.0000 6.750,1.2150,0.02344,0.01348,-0.0718,0.3682,1.0000 7.000,1.2385,0.02406,0.01406,-0.0712,0.3593,1.0000 7.250,1.2617,0.02480,0.01479,-0.0706,0.3515,1.0000 7.500,1.2851,0.02549,0.01547,-0.0700,0.3437,1.0000 7.750,1.3092,0.02630,0.01624,-0.0696,0.3370,1.0000 8.000,1.3303,0.02709,0.01713,-0.0688,0.3297,1.0000 8.500,1.3749,0.02882,0.01892,-0.0676,0.3166,1.0000 8.750,1.3984,0.02965,0.01976,-0.0671,0.3105,1.0000 9.000,1.4222,0.03068,0.02078,-0.0668,0.3049,1.0000 9.250,1.4387,0.03172,0.02204,-0.0655,0.2986,1.0000 9.500,1.4639,0.03257,0.02283,-0.0653,0.2926,1.0000 9.750,1.4813,0.03381,0.02423,-0.0642,0.2868,1.0000 10.000,1.4976,0.03495,0.02554,-0.0629,0.2808,1.0000 10.250,1.5242,0.03595,0.02644,-0.0630,0.2756,1.0000 10.500,1.5360,0.03748,0.02826,-0.0613,0.2703,1.0000 10.750,1.5493,0.03876,0.02972,-0.0598,0.2645,1.0000 11.000,1.5767,0.03973,0.03058,-0.0600,0.2592,1.0000 11.250,1.5821,0.04155,0.03271,-0.0577,0.2543,1.0000 11.500,1.5906,0.04301,0.03440,-0.0557,0.2488,1.0000 11.750,1.6186,0.04376,0.03503,-0.0559,0.2432,1.0000 12.000,1.6185,0.04580,0.03736,-0.0532,0.2387,1.0000 12.250,1.6180,0.04763,0.03946,-0.0505,0.2339,1.0000 12.500,1.6363,0.04864,0.04048,-0.0497,0.2290,1.0000 12.750,1.6525,0.05028,0.04218,-0.0489,0.2247,1.0000 13.000,1.6267,0.05313,0.04541,-0.0440,0.2218,1.0000 13.250,1.6049,0.05603,0.04857,-0.0400,0.2188,1.0000 13.500,1.6087,0.05775,0.05039,-0.0383,0.2148,1.0000 13.750,1.3936,0.08067,0.07403,-0.0368,0.2183,1.0000 14.000,1.3997,0.08285,0.07627,-0.0365,0.2143,1.0000